YANG Qian-long, ZHOU Feng-qi. Semi-physical Simulation of the Gliding Missile Flight Control System Based on Windows Operation System[J]. Microelectronics & Computer, 2012, 29(4): 154-157.
Citation: YANG Qian-long, ZHOU Feng-qi. Semi-physical Simulation of the Gliding Missile Flight Control System Based on Windows Operation System[J]. Microelectronics & Computer, 2012, 29(4): 154-157.

Semi-physical Simulation of the Gliding Missile Flight Control System Based on Windows Operation System

  • A semi-physical simulation platform in use of windows operation system is successfully established bases on general industrial PC combined with an external timer,the precise timing and steady multithreading serial communication are realized.The system is proved satisfying the real-time simulation requirement of the gliding missile.The novel platform could not only low-cost,but also is precise and universal,which has been successfully used in the semi-physical simulation practice of a gliding missile.
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